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dc.contributor.authorChen, Beixi
dc.contributor.authorWang, Kan
dc.contributor.authorEl-Mowafy, Ahmed
dc.contributor.authorYang, Xuhai
dc.date.accessioned2024-03-18T00:25:34Z
dc.date.available2024-03-18T00:25:34Z
dc.date.issued2024
dc.identifier.citationChen, B. and Wang, K. and El-Mowafy, A. and Yang, X. 2024. Real-Time GNSS satellite SISRE and its integrity for LEO satellite POD. In Proceedings of 2024 International Technical Meeting of The Institute of Navigation, 23 - 25 Jan 2024, Long Beach, California.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/94523
dc.description.abstract

The real-time Global Navigation Satellite System (GNSS) precise orbital and clock products are essential prerequisites for the Positioning, Navigation, and Timing (PNT) services and have been assessed in various studies. Compared to the precision of the orbital and clock products, their combined effect expressed in Signal-In-Space Ranging Error (SISRE) is of higher concern for positioning users. As a special user of the GNSS, the Low Earth Orbit (LEO) satellites need high-precision real-time GNSS products for their Precise Orbit Determination (POD) and clock determination in real time, which enables the future LEO-augmented GNSS PNT service. This study performs a comprehensive analysis of the real-time GNSS products from five different analysis centers, including analysis of their continuity, accuracy of their orbits, precision of their clocks, and their SISREs for LEO satellites at different altitudes. Using the tested products, the LEO POD was also performed to verify the correlation between the quality of the GNSS products and the accuracy of the LEO POD. Furthermore, to assess the integrity of real-time GNSS products, the overbounding standard deviations and mean values of the combined clock and orbital errors were computed and compared for different institutions. It was found that the GPS and Galileo SISRE range from a few centimeters to around 8 cm, while the SISRE of the Beidou Satellite Navigation System (BDS) Medium Earth Orbit (MEO) is a bit worse, i.e., around 1-2 dm. It has been demonstrated that there exists a positive correlation between the SISRE and user altitude, which implies a higher bias introduced to LEO satellites than ground users. The overbounding standard deviations and mean values of the GPS and Galileo products are all within 1 dm, whereas for BDS they are about 1-2 dm. Among the tested products, the smallest SISRE and overbounding values were delivered by the National Centre for Space Studies (CNES) in France for GPS and Galileo, while the GNSS Research Center of Wuhan University (WHU) provided the best accuracy and integrity for the BDS MEO products.

dc.relation.sponsoredbyhttp://purl.org/au-research/grants/arc/DP190102444
dc.subjectLeo, GNSS, Orbits
dc.subjectIntegrity monitoring
dc.titleReal-Time GNSS satellite SISRE and its integrity for LEO satellite POD
dc.typeConference Paper
dcterms.source.startPage807
dcterms.source.endPage820
dcterms.source.titleProceedings of the 2024 International Technical Meeting of The Institute of Navigation
dcterms.source.conference2024 International Technical Meeting of The Institute of Navigation
dcterms.source.conference-start-date23 Jan 2024
dcterms.source.conferencelocationLong Beach, California
dc.date.updated2024-03-18T00:25:33Z
curtin.departmentSchool of Earth and Planetary Sciences (EPS)
curtin.accessStatusOpen access
curtin.facultyFaculty of Science and Engineering
curtin.contributor.orcidEl-Mowafy, Ahmed [0000-0001-7060-4123]
dcterms.source.conference-end-date25 Jan 2024
curtin.contributor.scopusauthoridEl-Mowafy, Ahmed [7004059531]
curtin.repositoryagreementV3


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